Flow controlling mechanism for reaction type motors



T. M. LONG Jan. 27, 1959 FLOW CONTROLLING MECHANISM FOR REACTION TYPE MOTORS Filed June 12, 1947 4 sheets-sheet 1 JNVENTOR. A Wiz/dared [013g y .dull/4. MVH ILIv' T. M. LONG Jan. 27, l1959 FLow CONTROLLING MEcHANrs-M FOR REACTION TYPE MOTORS Filed June 12, 1947 4 Sheets-Sheet 2 INI/ENTOR. Tl/wlan 1% Zn BY vdab@ anw( H TTPNEYS T. M. LONG Jan. 27, 1959 FLOW CONTROLLING MECHANISM FOR REACTION TYPE MOTORS Filed June l2, 194'? 4 Sheets-Sheet 3 INVENTOR. Mr// JM [my WM M Jan. 27, 1959 T. M. LONG 2,870,603

FLOW CONTROLLING MECHANISM FOR REACTION TYPEMOTORS Filed June l2, 1947 4 Sheets-Sheet 4 l f 7a t /Z A 74 I j@ IN VEN TOR. 55 17m/mf# w1 f' JZ I BYMa/WL United States Patent O FLOW coNrRoLLI'NG MECHANISM Fok REACTION TYPE MOTORS Theodore M. Long, Somerville, N. J. Application June 12, 1947, Serial No. 74,133 zo Claims. (ci. 60s-35,6)

This invention'relates to a structurally and functionally improved flow controlling mechanism and in its more specific aspects aims to provide a unit embracing a variable area orifice injector which may be used in numerou different associations.

Such associations may, for example, be the mixing of liquids, gases, powdered solids or suspensions in chemical processes when mixing and/or ne atomization are necessary. Additionally, the unit may in certain instances be employed advantageously in connection with combustion chambers such as those of gas turbines, jet engines and internal combustion engines. However, in certain respects the present controller is` primarily intended for employment with a rocket motor in which connection it will-in the following specication-be described.

Therefore, it will be understood that this description is to be taken in an illustrative rather than a limiting sense except where the annexed claims indicate a cont'raryv conclusion.

Thus, it is a primary object of the invention to provide a controlling structure in association with or forming a part of a liquidl rocket motor injector and lwhich structure will be capable of throttling the rocket motor atV constant inlet pressures by Varying the areas ,of the injection orifices and the nozzle area ratios, while at the same time, maintaining a definite relationship between the throttling produced by each. Accordingly, optimum value of the design characteristics will be obtained by maintaining a substantially constantchamber pressure.

' A further object is thatv of providing in arocket motor ades'ired relationship between the oxidizer injection rate, thev fuel injection rate and the nozzle area ratios.

Another object is that of` furnishing acontrollenin which the parts may be adjusted so that the ratio be-k tween the fuel and oxidizer injectionv rates may be varied with respect to the nozzle area ratios and each other. Accordingly, a functioning of the motor occursunder conditions of maximum eliciency.

A still further object is that of providing a control for governing the mixing of, for example, an oXidizer and fuel and in whichvthe areas of both the converging andr the' diverging sections of the nozzle may be maintained under substantially constant contraction andl expansion rates. Thus, the variation in area is made in a different relationship with the' areas of the injection orices to produce a high jet velocity andl chamber pressure at a l'ow thrust output. In a different relation, the nozzle expansion ratios may be altered in anothermanner soas to maintain, efficiency with variation inaltitude, thrust; or both.

Still another object is'thatV of providing a structureof this type and in which, for example, a simple switch assembly permits'of complete controlof therocket motor consistent with any given inlet pressure.'A

An additional object is that" of furnishing a mechanism ofi thisrcha'r'acter whichlwill embody relatively fewy parte,

each"i`ridividually"simple and rggedinconst'ruction", these 2,870,603 Patented Jan. 27, 1959 ice 2 parts operating over long periods of time with feedlii from all diiliculties;

With these and other objects in mind, lreference is had to the attached sheets of drawings illustrating practical ein bodiinents of the invention, and in which Fig. 1 is a partly fragmentary side elevation of iiitor mechanism for a rocket and including the present ciil troller structure; v i

Fig. 2 is a sectional side View of certain of the vparte as illustrated in Fig. 1 but showing the ssrii iii diirsiiit position; 1

Fig. 3 is` a rear elevation of the apparatus as shown iii Figs. 1 and 2;

Fig. 4 is a transverse sectional view taken along liiies 4 4 as indicated in Fig'. 2;

Fig. 5 is a sectional side View of one forni of the coiitroller mechanism;

Fig. 6 is an end lView taken along lines 6--6 and in the direction of the arrows as indicated in Fig. 5;

Fig. 7 is a transverse sectional view taken along line 7 7l and in the direction of the arrows as indicated iii Fig- 5;

Fig. s is ajvisw schematically iutististiiig a lsyiitef apparatus such as may be employed in a rocket iiistalltion;

Fig. 9 is a' somewhat enlarged fragmentary' sectional side' view of 'certain of the parts as shown especially( iii Fis# 2; .4

Pig.l 10 is a transverse sectionalview takeh along linee 10Q-10 and in the direction of the arrows' as' indicated iiil rig.` 9;

Fig. 11 is a view of a layouto'f mechanism as generallyl shown in Fig. 2 but embracing nodiverg'ng restriction structure;

Fig. 12 is a sectional side View similar t Fig. 5 buf showingI a structure which' may be employed if sepate cooling isv to be utilized;

Fig. 1'3 shows anI arrangement f partse'mbr'acig the` injector' and controls therefor but in which no associated restrictor is employed; and

Fig.- 14Y is a view schematically/showing a' circuit of i electric motor which may operate the mechanism.

Referring primarily to a general layout df parts stitit as is illustrated in Fig'. 8, it will be seen that the reference numeral indicatesl anair-supply flask from' which a line Zmay extend. Within this line' a riianually controllable valve 3iV may' be interposed asA may also an air-regulatorvalve 4. Beyond this point, branches may connect uns z with a fusi tank s r'rd an oxidizsr tarik' 6 fromwhich lines 7 and 8 leadl towards the control'mechanism: As" shown, valves- 8' may interposed inY both the oxidizer line 7 and fuel tank line 8, These valves would` be the main propellant valves. Ordinarily, they would only bel capable of being thrown to providel either fully' opened or closed positions; The propellant-'contrll'ingf valves may be operated in any desired manner. The line 8 may terminatel in a ilexible portion of c'oilpliri'g'I 9'; the purpose of which willl be hei'nafter described@ As will be understood by those conversant with the art, the flask 1 may, for' example, be charged to proV al sourceY of air supply at 2,000l pounds per square inel. The regulator valvev 4 may, forv example, reduce pressureto 50o pounds: The' lirt's 2 bsirig c'oiiiis'ct'd te tanks 5 and 6, the air under pressure` will serve to expel fuel and oxidizer from these tanks into the lines 7 and 8.;

With the Valves in such latter lines open, the fuel and onefor'r'iof structure with which controllers constructed 4 1 in accordance with the present teachings maybe connected.

`Now referring to the detailed structures of the controllers-orinjectors, it is primarily -to be understood that in the following 'description certain passages will be referred to as providing paths for the flow of oxidizer. Others will provide paths fortheow of fuel. yIn most instances, the `reverse might be true. Therefore, these passages are to be considered as interchangeable. Also, only in one of thel lforms herein illustrated has there been included a structure providing for cooling of the injector mechanism, per se. As will again be understood by those skilled in the art, suitable cooling passages might be'includid in any of the structures hereinafter described.

Thus, referring to Fig. 5 inwhich one form of controller has been illustrated, it will be seen that the numeral indicates a casing which may be made of any suitable number of parts, properly vcoupled to each other in any desired manner. Therear portion 11 of this casing is formed with openings 12 conveniently ldisposed in an annular series and through which the oxidizer will ow in a manner hereinafter brought out. The rear wall of the casing portion 11 presents an opening conveniently defined by a surface 13 which provides a valve seat. A

retainer 14 may conveniently secure the casing portions 10 and 11 against separation and packing such as indicated at 15 may be provided to prevent undesired escape of uids at this or other points within the mechanism.

`Disposed within the casing portion 11 is a valve 16. This valve is cooperable with the `seat 13 and is provided with a central bore 17. Controlling the flow of uids through the bore 17 is an inner valve seat 18. This seat is `in the form of a head from which a shank portion extends in an axial direction. The shank portion mounts a retainer 19 against which a spring 20 acts. A stop 21 limits movement of the shank and seat portion 18 to the right asin Fig. 5. A packing 22`may be disposed beyond the stop 21 and beyond which a retainer 23 is disposed. A body 24 may enclose the several parts of this assembly as well as a thrust bearing 25 disposed beyond that assembly. Enclosed by the shank of the inner valve seat 18 and extending through the several parts disposed adjacent the inner end of the same is a restrictor rod and drive screw assembly or member 26. As shown, this member is formed with a bore for the passage of fuel and with ports 27. It is interrupted, as'in Fig. 7, to permit of fluid ow from its bore through these ports. While the ports 27 Ymay involve `any desired construction, they are preferably in the formv (as shown) of a peripheral slot cut in the outer wall of the restrictor-rodl and drive screw assembly. Thus, the port or opening will cover a full 3 60" of the restrictor rod. Therefore, as the rod rotates within the inner valve seat 18 (which is stationary) the port area will not be momentarily closed so as to partially restrict the fluid transfer. In this connection it is apparent that partial or momentary closure would occur during part of the rotation if any of the outer Walls of the rod were left at this zone. Accordingly, fuel may ow from the bore of member 26 into the space between the inner valve seat 18 and the valve 16. An escape of fuel from this space other than past the seat 18l is prevented by an enveloping member 28 which may be in the form of a bellows seal; suitable packings 29 securing the ends of the seal or enveloping element in uid tight relationship with respect to adjacent parts.

movement of the parts with respect to each other is conveniently effected by employing a motor 30. The latter serves to actuate a drive gear 31, the teeth of which mesh with a gear 32 having a rearwardly extending sleeve 33. This sleeve has radially extending teeth 34 formed on its outer face and which are engaged by the' shafts 36 terminate in threaded portions 38 and 39. The threads of these different portions may, for example, both be right hand. However, their pitch is different. The threads of the left hand portion 39 may engage with correspondingly threaded sockets 40 formed in the inner face of valve 16. The right hand or inner thread portions 38 may engage with correspondingly threaded bores formed in the body 24. The rod 26 is conveniently formed with splines 41 upon which a spacer 42 is disposed. The inner end of this spacer engages a thrust bearing 43 beyond which is arranged a cap 44. This cap has a threaded bore engaged by the threads 45 of the rod 26.

At this time, the ,motions imparted to these elements of the mechanism should be considered. The amount of movement specified may, of course, be varied. However,

a general relationship as indicated is preferably to be- Inother words, for each rotation al movement of .022" inch occurs.

Therefore, forv each turn, a travel of .0 20 inch occfu'rs.rv The advance imparted by threads 39 withrelation to the' axial movement of rod 26 is '.022. However, valve 16 i will advanceonly .022A inch'minus .020 inch. Therefore,

for each turn valve 16' advances only a distance of-.002 inch. M

The stop member 21 is adjusted so that the seat` 18 initially moves with the valve 16 as the parts shift to theY right. However, this engagement of the'parts may vfollow through only a distance of .0001 inch. Such travel may, under certain conditions, be in excess of the latter ligure but movement in unison should not occur through too great a distance. After such movementhas been completed, the seat 18 will remain stationary while valve" 16 continues to travel. Therefore, with valve lrmoving' a maximum distance of .O50 inch, it follows that if the,

unison travel of 16 and 18 is .0.001 inchfthatthe maximum separation of these elements will be substantially .049 inch which may, of course, beless if vthe stop 21 is adjusted to provide a dilferentresult. f

A casing 46 extends rearwardly from the outer valve seat member 11. Having in mind that the present 'ap-k paratus is primarily intended as a controlling mechanisml for useY with a jet or rocket motor, this casing 46v is ex-V tended inwardly and outwardly to providenozzlecones 47. Disposed adjacent theV innermost of these cones and Within the casing 46 is a converging restrictor 48. D'islr posed for proper cooperation with theoutermost cone is a diverging restrictor 49. The casing may vterminate 51 are mounted for slidable movement.

restrictor supporting arms 54 whichl are connected to the manifold are hollow so that fuel may ow fromthe manifold inwardly through the arms and through-ports to the bore of the restrictor r0'd26. As will be under-k stood the rod designated at 26 is actuallyan assembly includingboth outer and inner members. This assembly: is continued inthe 'form of the diverging restrictorj48,

and has@ s.

Threads 38 which' conveniently include fifty operative convolutions provide for a movement of The interior of thevdivergingrestrictor .49 is-threaded and` engaged. by they correspondinglythreadedV exterior oft the rod assembly 26 as indicated'atSS in Fig.. 21 Such threading is. preferably of relatively high pitch. A restrictor insert 56 is disposed within the bore of the diverging restrictor and a restrictor. seal S7 secured by a retainer 58 prevents an escape of fuel. A bafe 59 is. disposed within. the converging restrictor 48A and formsv a part of the assembly 26 asafore described. The baffle may terminate in an extended portion. 60` providing a guide, as in Figs. 2, 9`andl 10. This. portion will also function as a flow accelerating member. Guides. 61 may be interposed between the-.restrictor annulus and the rod assembly 26 and be continuedV as parts interposed between thc converging restrictor 48 and the` baille 59.

As afore brought out, the rod 26 in the example previously given moves a distance` of 1.25 inches. Therefore the converging restrictor 48 andv baffle 59 will have acorresponding'movement. However, the. threads 55 will provide for a movement onv the. part of the diverging restrictor 49 of one and. one half inches or more in the opposite. direction. It should be remembered,v that the restrictors 48 and 49 always move in. opposite directions. Therefore, if rod 26 is rotated 25 times, the converging restrictor 48 will be shifted the desired amount. by the threads 45. Simultaneously, the threadsSS. will shift the diverging restrictor 49 the required amount.

As indicated especially in Fig. 1, the inner end of the rod 26 may carry a limit switch plate 62. This mayl engage the normally closed limit switches 63 and 64 to open the same. These switches-prevent. the motor 3.0. from operating the parts beyond predetermined. limits. That motor may be of any suitable type involving proper circuits and controls resulting ina desired` functioning, ofv the parts. AsV shown the predetermined. limit under which 63 opens may be that in which. the valve 16 (as in;Fig. 5) is in the extreme left. position as hereinafter described. The predetermined position under which` switch. 64.opens may be any one convenient to the operation of the mechanism. Within these limits and referring toFig. 14, the master switch may be thrown to= the left. completing the circuit from a direct current. power supply through limit switch 63. The polarity, of. the: power supply and the. connectionsv of. the interior parts of the motor, the armature, the shunttield and the series field are such that motor 3). operates the rod 26v in. clockwise rotation to the leftiuntil themaster switch isopened or untilthe limit switch. 63 is opened by contact withlimit switchplate 62. Similarly, closing themaster switch to the right asin. Fig. 14 will interchange. the.- connectionsof the interior parts of the-.motor and. complete the circuits. through limitswitch 64 causing. themotor to rotate in a direction opposite to that afore described. This will have the result of operating'the rod 26' in counterclockwise rotation tothe right as in` Fig.v 1v until themaster switch. is open or. until-*limit switch 64- is. opened by Contact of the limit. switch plate 62. As will also be understood, the motor drive of the gear 31 could be supplanted by any other desired formcf drive as could also the detailed transmission. of power by the gear 32,. the gears driventhereby, etc. v

Withvalve 16 in an extremey left` position as. viewed iniFig. 5, it is apparent that this valve will engage seat 13 as well as seat 18. Under theselcircumstances, noy oxidizer. or fuel fluid will .ow through the outlets. However, as the shafts 36: are rotated, valve 16v will be movedv from its seat 1310. allow of a iiow` of. oxidizer through` ports 12' and sopast the seat 13. In such initial movement of the ports, the head 18' of the4 second valve seat Willmove with the valve 16. This. will be because of the spring 2t). Withr the valve 16 continuing to move in thedirection specied, it: willas aforebrought. 'outunseat from the member. 18. Consequently fuel. may flow. throughy the. bores of. the restrictors and drive rod 26 past. the. interrupted portion of i that. assembly and 6 through the ports 27. As,previously mentione.dan. inteimingling of theoxidi'zer and fuel' will be preventedby the several packingsand especially the bellows seal 28.-

It will, of course, be understood that the fuel. enters through the tubes 9 and 53, manifold. 521 and the fuel inlet passages through the restrictor supports 54. After passing from these supports, the fuel flows through the interior of the restrictor insert S6 and then passes into the interior of the restrictor annulus where it is forced to flow evenly and with considerable velocity by means of the extension 60, the restrictor baffle 59V and guides 61. In this manner the fuel is used to cool the complete-rej strictor assembly. Thereafter, and as. afore brought out,

the fuel enters the. fuel annulus. r

As is apparent, the converging restrictor 48 controls. the converging section of the nozzle. The divergingre'- strictor 49 controls the area of the diverging section of the nozzle. Restrictor 48 is connected by means of the rod 26 to move in the. same direction as. the valve 16. Restrictor 49 moves in an opposite direction, by virtue of the fact that it is maintained by the guides 5.0, the manifold 52 and incidental structures against rotation and because of the screw threads 55. Therefore, with. the restrictors moving in an opposite direction, the fuel and oxidizer injection rates are reduced when the areas ofthe converging and diverging sections of the nozzle are reduced. When moved in an` opposite direction, the injec-A tion rates and areas increase simultaneously. The two restrictors are so contoured that the ratio of the area2 of the convergingl section to the areas of the diverging section 'remain nearly constant when so desired.. This. will maintain nozzle and combustion` eiciency over ai large range of the thrust output. In another relationshipy betweenV injection rates and restrictor configurations the parts may be specifically designed tol increase efficiency at low'thrusts at high altitudes.

In certaininstances, -it may not be necessary or desirable to use the diverging restrictor. Such an arrangement has been somewhat schematically illustrated in Fig. 1l. In that view, the numeral 65 indicates the rod..cor. responding to the rod assembly 26 in the earlier views. The numeral 66 indicates the valve corresponding vto',l valve 13. AdjacentL structures have not beenyshown in. this view in that it maybe assumed that-functionally theyE are duplicates. of they mechanisms heretofore described. Ports 67 may be provided to furnish communication be-A tween the bore of the rod and thel parts exterior thereto; Adjacent its rear end, this rod 65 or a continuation thereof terminates in a baiiie portion 68havinga rear open;

end 69. Concentrically disposed with respect tol this baffmanner indicated by thev arrow through. the bore of rodi,

65. This iiow will. continue through. thediverg'ing restrictor 68 and outwardly through the rear. end ofv the same. Thereupon the yflow will reverse. through the space intervening the restrictor and. bafe: and will continue; the

uid escaping through the-ports'67 or-otherv desired` out- As is apparent incident tofsuchfl'ow. arcooling of As will.' also.- be'i app'arent,. the rod:

let. the parts will occur.

65'may either benen-rotatably. supported (as inthe case'. of the rod hereinafter described.inFig,.12.) or` this'rod` may be rotatable;

inthe'r form' of construction shown inFig. l-2.a mecha-A nism generally. similar t'o that heretofore described? in: Fig. 5 has been shown;

spending parts Wherever this has been.practicable.v How-- ever, as will primarily be notedwithregards to' this structure, a tube 73 may be. coupled to a passage'74 formedin the body 7,5 of. the unit. This passagerwillservertoj For. 'this reason, similar refer# encey numerals' have been employed to designate corre- :garderie provide a path of flow for the fuel such that it may pass through'one or more passages A76 to the central bore 17. `In this form of construction, it is feasible to provide for separate cooling for the restrictor or restrictors. To this end, a suitable cooling agent (other than the fuel or oxidizer) is introduced into the inner restrictor passage and may be allowed to escape by way of the outer restrictor passage. f

More particularly, the rod assembly 77 will provide for these passages as shown in this figure. This assemlbly may be non-rotative and limited solely to an axial Shifting. As will be apparent in this connection, the mot'or 30 may drive gear 78. The teeth of the latter engage the teeth of a gear 79. The latter gear is formed with a bore which is interiorly threaded to furnish in effect a nut. These threads engage with threads 80 on `the rod assembly 77. Any suitable number of shafts 81 similar to shafts 36 may be employed and which mount gears 82 meshing with the teeth of gear 79. Suitable bearings 83 may also be provided to absorb the thrust strains which are present.

As will be obvious, a rotation of the gear 78 will cause a corresponding movement on the part of gear 79. As-

suming'that the rod assembly 77 is maintained against rotation (by for example, a spline 77'), then it is apparent that the rotation of gear 79 will cause the rod assem- `bly to be shifted axially. With such shifting, the restrictor may be'correspondingly moved. Also, the shafts 81 will be simultaneously rotated to assure an operation of `the valve 16 in a manner heretofore described.

Finally, there has been shown in Fig. 13 a relatively fv'cry simple embodiment of structure designed in accordance with the teachings of the present invention. In that view, a tubular member S4 is substituted for the rod assemblies heretofore described.` In any suitable manner, lgear 85 may be driven. This will serve to drive a gear 86, the teeth of which engage with any proper number of gears 87. The latter are mounted on shafts S8 corre-` sponding to the shafts 36 and 8l; Bearings 89 may be provided as may also the heretofore described adjustable stop, spring, etc. for the valve 90 which corresponds to the valve 16. The seat member 91 may have the usual extended portion 92 and have the bore of such portion `in communication with the bore of tube 84.

Thus, fluid will be free to flow through the tube of the `latter bore and into the bore of extension 92. As the igear 85 is operated, gears 37 will be caused to rotate. l'1` his will drive shafts S8. Therefore, in a manner similar `to that heretofore described, the valve 90 will be caused `toseat and unseat both with respect to the body 11 as well as the member 91. Accordingly, flows of fluid as also heretofore described, will occur. y From the vforegoing it Will be understood that among `others the several objects of the invention as specifically afore noted are achieved. Obviously numerous changes in construction and rearrangement of the parts may be resorted to without departing from the spirit of the invention as defined by the claims.

What I claim is:

l. A flow controlling mechanism for reaction type motors having a combustion chamber, said mechanism including in combination a converging-diverging nozzle, a body in advancev thereof and connected thereto, said body providing a valve seat, a valve movable with respectthereto and provided with a bore, said body being also provided with a bore, one of said bores serving as a passage for. the flow of fluid oxidizer and the other for the flow of fuel, a further valve seat cooperable with `said valve for closing the bore of the latter -against the flow of uidtherethrough, means for shifting said valve into-and out of seating engagement with its seats, the proportioning of said valve seat and further valve seat together with the establishment of desired pressure differentials in said fluids across sadvalve seat and further valve seatserving to meter the owbfoxidizer and fuel in idesiredvratio of one to the other Vwhen said bores are partiallyY obstructed by said valve and the proportioning :of said valve seat and further valve seat serving to inject and mingle ,the said fluidsfor combustion insaid combustion chamber. K i

2. A flow controlling mechanism for reaction type motors having a combustion chamber, said mechanism including in combination a converging-diverging nozzle, a body in advancethereof and connected thereto, said body providing a valve seat, a valve movablev with respect thereto and provided Withy a bo're, said body being also'provided with a bore, one of said bores serving as a passage for the flow of fluid oxidizer and the other for the flow of fuel, a further valve seat cooperable withsaid valve for closingthe bore of the latter against the flow of fluid therethrough, Imeans for movably mounting saidv further' valve seat, means for shifting saidvalve into and out of sealing engagement with the valve seat provided by said body'and means for limiting the flowrestricting movement of said further valve seat.- y

3. AV ow controlling mechanism for reaction type motors having a combustion chamber, said mechanism including in combination a converging-diverging nozzle,

body in advance Athereof and connected thereto, said body providing a valve seat, a valve movable with re spect thereto and provided with a bore, said body being also provided with a bore, one of saidv bores serving asaij'passage for the flow of fluid oxidizer and theother for'the flow of fuel, a further valve seat cooperable with said valve for closing the bore of the latter againstV the flow of fluid therethrough, means for shifting said valve into and out of sealing engagement with its seats and a flexible sealing member extending between Vsaid valve and body to prevent a mixing of the combustible propellents prior to theirintermingling in the combustion chamber of the apparatus. Y l

v4. A flow controlling mechanism for reaction type motors having a combustion chamber, said mechanism including in combination a converging-diverging nozzle, a body in advance thereof and connected thereto, said body providing a valve seat, a valve movable with re' spect thereto and provided with a bore, said body being also provided with a bore, one of said bores serving as a passage for the'flow of fluid oxidizer and the votherv for the'flow of fuel, a further valve seat cooperable with said valve for closing the bore of the latter againstthe flow of fluid therethrough'means for movably mounting said further valve seat, kmeans for shifting said valve into and out of sealing engagement with the valve seat provided by said body, a spring for urging said further valve seat in a flow-'interrupting direction and an ad-l justable stop'for limiting schmovement. f 5.*A ow controlling vmechanism for reaction typ motors having a combustion chamber, said mechanism including in combination a convergingdiverging nozzle, a body in advance thereof and connected thereto, said body providingl a valve seat, Ya valve movable with respect thereto and provided with a bore, said body being also provided with a bore, one of said bores serving as a passage for the flow of fluid oxidizer and the other' for the flow of fuel,` a further valve seat cooperable ywith s aid valve for closing the bore of the latter kagainstthe flow of fluid therethrough, means for shiftingsaidvalve into and out of sealing engagement withits seats, a

restrictor rod operating within said converging-diverging nozzle and a drive assembly connected to, movable with and extending beyond said further valve seat.

' 6. AA flow controlling mechanism for `reaction type motors having a combustion chamber, said structure in# cluding in combination a nozzle having converging-di` verging sections, valve means governing ,the flows of fluid fuel andoxidizer, a restrictor having surfaces'disposvable adjacent and cooperative with the sections of said nozzle, said restrictor being connectedsto said'valve means, common 'means for simultaneously` shiftingfsaid valve means and restrietor, hollow supports connectedy to said restrictor, means coupled to said supports and providing a path for the ow of` fluid fuels and guide means cooperable with said support to prevent rotation thereof and also prevent rotation of said restrictor while supportingk said restrictor for axial movements within the sections of saidy converging-diverging.,nozzlefto cause a variation in the area of the sections: of said-converging-l diverging nozzle.

7. A ilow controlling mechanism for reaction` type motors having a combustion chamber, saidmechanism including in combination a converging-diverging nozzle, a. body in advance thereof and connected thereto, said body providing ay valve seat a` valveA movable with respect` thereto andprovided with a. bore,- said body being also provided with a bore, one of saidbores serving as aY passage for the flow of, uidf oxidizer and. the other for the flow of fuel, a further valve seat-cooperable with said valve for closing. the bore of the latter against the flow of fluid therethrough,v saidvalve beingformed with screw threadedA openings, a' plurality of screw threaded rods extending into said openings and through openings in said' body, said latter openings. havingy their'surfaces also threaded and pitched in a-` direction similar to but toI a lesser degree than said screw threadedopenings in saidf valve and means for rotating said rod: to' provide al differential screw actionv suchthat said valve` will be moved into engagement with its seat-to` interrupt aow of uids'through both of saidbores'.

8e A- flow controlling' mechanism for reaction type motors having acombustion chamber within whiclrfluid propellants are to be burned, said mechanism? including in combinationa converging-diverging nozzle,- abody in advance thereof andv connected thereto, said body providing: a valve seatV member, means for movably supporting the same, a; movably mounted valve` concentricallydisposed with respect to said member and formed with a-surfaee cooperable with the seat thereof, a' further bodyl concentrically' disposed with respect tosaid valve and also provided with a seat cooperable with a` further surface of said valve, the propellants owing past said seats towards said chamber, means` for moving said valve with respect to said member and further body and flexible sealing means extending' between said: member and further body to prevent the mixing of the propellents flowing past said valve seats. v

9. A ow controlling' mechanism for reaction type motors' having a combustion chamber, said mechanismincluding in combination' a' converging-diverging"nozzle, a body in advance' thereof and' connected thereto, said body providingaY valve' seatv member,l means for movably supporting the' same; a m'ovab'ly mounted valve lconcentrically disposed with' respect to'said Inem'ber and formed with' a' surface coop'erable with' the seats thereoi'a' further' body concentrically' disposed' with respectto" said valve and' alsov provided' with' a' seat 'cooperable' with a further' surface of `said' valve, means for moving said valve with respect'v tol said member and further body, a corrugated flexible seal element having its oppositeedges secured to said body and valve respectively to prevent a mixing of combustible?proponents ilow respectively between said valveandl fur-ther bodyyand saidvalve and seat member.

10. A ow controlling mechanism for reaction type motors having a combustion chamber, said mechanism including in combination a converging-diverging nozzle, a body in advance thereof and connected thereto, said body providing a valve seat member, means for movably supporting the same, a movably mounted valve concentrically disposed with respect to said member and formed with a surface cooperable with the seat thereof, a further body coneentrically dispoed with respect to said valve and also provided with a seat cooperable with a further surface` of said valve, a yiexible seal element extendingl between said body and said valve to prevent y12.0 almixing of fluids from the spacesintervening saidavalve and further body to the space interVeningsaidvalve andseat member and means. for moving said valve and connected to the same Within the space defined by` said seal element.

ll. A ilow controlling mechanism for reaction type motors having a combustion chamber, said mechanism including in combination a converging-diverging nozzle, abody in advance thereof and connected thereto, said body providing a valve seat member, means for movablysupporting the same, a movably mounted valve conL centrically disposed with respect to said member and formedl with a surface cooperable with the seat'thereof', a body concentrically disposed with respect` to said valve and also providedy with a seat cooperable. with a` further surface of saidvalve, means for moving said valve-*withrespect to said memberand body, a restrictorrody and drive assembly extending through. said valve seat mem-` ber, means for shifting saidassembly, means connecting saidl shifting, means to simultaneously move said-valve in Synchronism therewith and. a restrictor securedf to said rod.

l2. A flow kcontrolling mechanism for reaction type motorsA having a combustion chamber, said mechanism including in combina-tion a converging-diverging nozzle, a body in advance thereof` and connected thereto, saidy bodyY providing a valveA seat member, means for movably supporting the same, a movably mounted valve lconcentrically disposed with respect to said member and formed with ay surface cooperable 'with the seat thereof, a body concentrieally disposed withirespect to said valve and' also provided with a seat cooperable with a` furthersurface ofsa'id valve,` means for moving said valvey with respect toy saidn member and body, said seat member being formed with a bore and with openings' aifordingpassage from said b'ore to the space' interveningk said member and' valve and a tubular fluid-conducting memberdisposed in line with and communicatingv with` said bore. 13. A ow controlling mechanism for reaction typej motors having a combustion chamber, said mechanism including in combination' a converging-diverging nozzle, a body in advance 'thereof and connected thereto, said body providing a valve seat member, means' for movably supporting' the same, a movablyv mounted valve concem trically disposed' with respect to said member and formed with asurface cooperable' with the seat thereof, ay bodyeoncentricall'y disposed with respect to said valve and also providedwith a seat cooperable with a fur-.ther sur-` face" of said valve, rnean's `for moving -said valve with respect to said member and body, a restrictorl rodl assembl'y: formed with threads on its exterior face to oper'-v ate within: saidA converging-diverging nozzle, an interio-rly threaded member' engagingsaidv threads and rotatable to shift said-` assembly in an axiai" direction and means for; connecting said'interiorly threaded member With said Vsimultaneously body i-nladvance'thereofriand connected' thereto, saidbody providing afvalli/esea1t',iar valve movable with respect-thereto and provided with a bore, said body' being also provided with a bore,.one of said bores serving as a passage for the flow of fluid oxidizer and the other for the flow l of fuel, a further valve seat cooperable with said valve for yclosing the bore of the latter against the ow of iluid thereto, means for shifting said valve into and out of sealing engagement with its seats, a rotatable Vrestrictorv taneously rotate the latter and shift said valve.

valve shifting means and with said assembly to simul- 15. A flow controlling mechanism for reaction type motors having a combustion'chamber, said mechanism including in combination al converging-diverging nozzle, a body 1n advance thereof and connected thereto, said body providing a valve seat, a valve movablewith respect thereto and provided with a bore, said body being also provided with a bore, one of said bores serving as a passage for the ow of fluid oxidizer and the other for the flow of fuel, a further valve seat cooperable with said valve ifor closing the bore of the latter against the How of Iiluid therethrough, means for shifting said valve into and out of sealing engagement with `its seats, a restrictor rod assembly 4connected to move simultaneously with the movements of said valve and converging and diverging lrestrictors connected to said rod; such interconnected restrictors being so proportioned as to meter the ow of ltors having a combustion chamber, said mechanism in`- cluding in combination a converging-diverging nozzle, a v `body in advance thereof and connected thereto, said body providing a valve seat, a valve movable with respect thereto and provided with a bore, said body being also provided with a bore, one of said bores serving as a `passage for the flow of fluid oxidizer and the other for the o'w'of fuel, a further valve seat cooperable with said valve for closing the bore of the latter against the flow of Huid therethrough, means for shifting said valve into ,and out of seating engagement with its seats, a restrictor lrod assembly connected to move simultaneously with the movements of said valve, converging -and diverging relstrictors connected to said vrod and means interconnecting the parts whereby said restrictors are moved towardsY and away from each other within said converging-divergiing nozzle as said rod is moved.

17. A ow controlling mechanism for reactlon type motors having a combustion chamber, said mechanism `including in combination a converging-diverging nozzle, fa body in advance thereof and connected thereto, said body providing a valve seat, a valve movable with respect JIhereto and provided with a bore, said body being also ,provided with a bore, one of said vbores serving as a passage for the flow of fluid oxidizer and the other for the ow of fuel, a further valve seat cooperable with Said valve for closing the bore of the latter against the ow of fluid therethrough, means for shifting said valve into `and out of sealing engagement Withits seats, a rod con'- nected to move as said valve is moved, and a converging :or .diverging restrictorl xedly secured to said rod to op- `motors having a combustion chamber, said mechanism thenow vof fueLa further valve seat cooperable with said valve-for closingthegborejof theylatter against the flow of ',uid therethrough, means vfor shifting said valve into and out of sealing Vengagementhwit-h its seats, a rod connectedtoemove as saidl valve is moved, a converging or diverging restrctor secured tosaid rod, said restrictor and, rod being hollow for the passage of' fluid and a baffle member disposed within said restrictor.

19. A ilow controlling mechanism for reaction type mo'- tors having a combustion chamber, said mechanism in-y cluding in combination a converging-diverging nozzle, a body in advance thereof and connected thereto, said body providing a valve seat, a valve movable with respect thereto and provided with a bore, said body being also provided withv a bore, one of said bores serving as a passage for allow of `uid oxidizer and the other for the ow of fuel, a further valveseat cooperable with said valve for closing the bore of the latter against the ow of fluid therethrough, means for shifting said valve into and outr of sealing engagement with its seats, a rod connected to move as-said Vvalve is moved, a converging or diverging restrictor secured to said rod, to operate within said convergingLdiverging nozzle, said restrictor and rod beingl hollow for the passage of fluid, a baiile member disposed Within said restrictor, said bale being also hollow and provided with an open end communicating with the interior of said restrictor whereby fluid may flow through said baffle, restrictor and hollow rod. y

20. A ilow controlling vmechanism for reaction type motors having -acombustion chamber, said mechanism including in combination 4a converging-diverging nozzle, a body in'advan'ce thereof and connected thereto, said body providing a valve seat, a valve cooperable with Said seat, means providing a second valve seat andA ow controlling means cooperable therewith, means for shifting said valve and ow-controllingmeans .with respect to their seats, a tubular rotatable restrictor rod, means for connecting said rod with said valve shifting means whereby, as the latter operates, said rod is rotated,-`a restrictor, means forrestraining the latter against rotation and screw threads between said restrictor and rod whereby as the latter is roincluding .in combination .a converging-diverging nozzle,` l

a-body in advance thereof and connected thereto, said ibody providing a valve seat, a valve movable with respect `thereto and provided with a bore, said body being yalso `provided withV a bore, one of said bores serving as a passage for theow of fluid oxidizer and the other for tated said restrictor will be shifted.

. References Cited in the le of this patent UNITED STATES'PATENTS 633,415 Batchelor Sept. 19,v 1899 1,013,640 Bryon Jan. 2,k 1912 1,056,432 McCloud Mar. 18, 1913 1,463,370 Mueller July 3l, 1923 1,556,227 Lemtas Oct. 6, 1925 1,707,541 Roth Apr. 2, 1929 1,732,097 Lemtais Oct. 15, 1929 1,975,635 Dunham Oct. 2,' 19,34 2,254,303 Nicholas sept. 2', 1941 2,310,516 Clark Feb. 9, :1943, 2,390,161l Mercier Dec. 4, 1,945y

K FOREIGN PATENTS f' 556,902 Germany Jan. 30,1930

OTHER'REPERENCES Astronautics, lissue of March 1944, pages 11-13. 

